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Publication numberUS5611295 A
Publication typeGrant
Application numberUS 08/536,003
Publication dateMar 18, 1997
Filing dateSep 29, 1995
Priority dateSep 29, 1995
Fee statusLapsed
Publication number08536003, 536003, US 5611295 A, US 5611295A, US-A-5611295, US5611295 A, US5611295A
InventorsLloyd J. Stables
Original AssigneeStables; Lloyd J.
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Anti-spin/turning enhancer for personal watercraft
US 5611295 A
Abstract
Two non-movable plates mounted on the outside rear of a personal watercraft, extending below the lower edge of the hull. These plates provide lateral resistance and prevent the hull from sliding out at the rear which could initiate a spin. As these plates move laterally while in a turn they are designed not to adhere to the water by vacuum. When returning to a straight course out of a turn, the necessity to over steer is greatly reduced and the momentary loss of control is eliminated. Being considerably more narrow than the O.E.M. sponsons which they replace, lift is reduced and the pump intake remains more deeply engaged thus providing more steering control during high speed turns and manuevers. The attributes mentioned above add greatly to the safety of operation of a personal watercraft.
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Claims(6)
I claim:
1. An anti-spin and steering enhancement devise for jet powered personal watercraft compromising of a pair of wedge shaped outer plates extending below the rear left and right edges of the hull and a pair of spacers between the outer plates and the hull and a means for fastening said plates securely to the hull.
2. The device of claim 1 said outer and inner plates are composed of high density polyethelene.
3. The device of claim 1 said outer plate is of a vortex creating textured or pebbled finish.
4. The device of claim 1 said outer plate is a smooth finish not capable of producing vortexes.
5. The device of claim 1 said outer plate is designed with the top and bottom edges being non-parallel forming a wedge with rounded corners which reduces lateral adhesion to moving water.
6. The device of claim 1 the said outer and inner plates are mounted by one of either thru bolting, secured to existing studs and secured to existing threaded inserts in the hull.
Description
BACKGROUND-FIELD OF INVENTION

This invention relates to an anti-spin device for improving the directional control of jet powered personal watercraft with V and semi-V hull configurations.

BACKGROUND-DISCUSSION OF PRIOR ART

Spin out is an inherent problem of personal watercraft due to their more forward center of gravity. This problem is especially visible when making high speed tight turns.

Side sliding was addressed in U.S. Pat. No. 5,235,926 to Jones on Aug. 17, 1993 where dual pivotally attached metal fins were mounted to the rear of a flat bottomed boat. This would seem to be a very logical approach for larger multi passenger boats with conventional cockpits. Because of the difference in nature between conventional boats and personal watercraft, specifically the closeness of the operator of a personal watercraft to the rear of the craft, a serious safety hazard would exist if a design of this type were used. An operator could easily fall back upon exposed metal fins causing severe injury.

A side slipping situation was also addressed in U.S. Pat. No. 5,313,907 to Hodges May 24, 1994 where rails were mounted along the bottom outside corner of the boat hull, extending downward. The rails in his FIGS. 9 & 10 extend approximately half the length of the hull. Although side slipping would be reduced, the steering capabilities would be seriously de-tuned as rails of this length would hold the craft in a straight course.

OBJECTS AND ADVANTAGES

Accordingly several objects and advantages of my invention are;

(a) to considerably reduce spin out during high speed turns

(b) to enhance steering control during and when coming out of a high speed turn.

(c) to eliminate the need to over-steer when coming out of a high speed turn

(d) to furnish a device which does not create a safety hazard because of its location and minimal extension away from and below the craft.

(e) to accomplish precise control in a turn without a device of such extended length that horsepower and speed are lost working against such a device.

(f) to furnish a device that is virtually indestructable requiring no maintenance for its protection from corrosion, delamination and color fading.

(g) to furnish a device that cannot be shattered or broken to a point that sharp edges would create a safety hazard

Further objects and advantages of my device will become more apparent from a consideration of the drawings and my ensuing description

DRAWING FIGS. 1-5

FIG. 1 is a side view of my anti-spin device-left assembly.

FIG. 2 is a top view of my anti-spin device-left assembly.

FIG. 3 is an end view of my anti-spin device-right assembly.

FIG. 4 is a right side view of a personal watercraft showing my anti-spin device and its relative mounting location.

FIG. 5 is a right rear view of personal watercraft showing my anti-spin device and its relative mounting location.

REFERENCE TO NUMERALS IN DRAWINGS

______________________________________10           outer plate11           inner plate12           mounting holes13           hull of watercraft14           radius-outer plate edge15           bottom edge of hull16           degree of angle17           reinforcement washer18           personal watercraft19           pebble textured finishR-1          radius 1R-2          radius 2R-3          radius 3R-4          radius 4______________________________________
DESCRIPTION OF INVENTION

FIG. 4 shows a side view of my device as mounted on the right side of a personal watercraft. The outer plate (10 in FIG. 3) is mounted to the hull (13 in FIG. 3) with the inner plate (11 in FIG. 3) mounted between it and the hull.

This embodiment consists of a pair of inner and outer plates (10 & 11 in FIG. 1) mounted on both sides of the craft. As shown in FIGS. 3, 4 & 5 the outer plate (10 in FIG. 1) will extend below the bottom outside edge of the hull (15 in FIG. 3) approximately one inch but is not limited to that dimension.

These devices are mounted to the hull using existing holes (12 in FIG. 3) from which O.E.M. sponsons were removed. These devices may also be stud mounted on existing studs from which O.E.M. sponsons were removed.

The fastening devices for mounting, for safety purposes, must not protrude more than 1/4 inch above the outer plane of the outer plate (10 in FIG. 1). It must be round and smooth in nature. As an example a carriage bolt or truss head bolt may be used. A hex head bolt may not be used. When stud mounting, the studs may not protrude thru the outer plate (10 in FIG. 1). As an example a stud may be shortened, a coupler nut added and a truss head screw screwed into the coupler nut thru the inner and outer plates (10, 11 in FIG. 1).

Because of so many variations in O.E.M. mounting and continual changes by O.E.M. manufacturers this inventor will suggest the best mounting application at a given time. I would not specify a given method at this time because it could become non-feasable at any time.

When possible, reinforcement such as large finishing washers (17 in FIG. 3) should be used inside the hull. Any additional reinforcement will be at the owners discretion. All hardware will be stainless steel and in no case smaller than 1/4 inch in diameter.

The outer and inner plates (10, 11 in FIG. 1) are manufactured from 1/2 inch thick high density polyethelene or similar material in sheet form. These devices are saw cut with the outer plates (10 in FIG. 1) being routed using a 0.20 in. router bit. they may also be injection moulded with the rounded outer edges formed by the mould. The surface of the outer plate (10 in FIG. 1) contains a moulded in pebbled finish (19 in FIG. 1 ). This finish contains approximately 1500 indentions per square inch at a depth of 0.015 inch.

The actual length of the assembly can vary from 18 to 30 inches coinciding with the length of the O.E.M. sponson which it replaces. The length of the backing plate (11 in FIG. 1) would be adjusted accordidngly. The radii (R1 thru R4 in FIG. 1) are as follows: R1--0.90 in. R2--6.75 in. R3--0.70 in R4--2.50 in. The angle (16 in FIG. 1) is 52 degrees. The outer plate (10 in FIG. 1) is 2.25 inches high at the front, measured from the beginning of the top flat to the extended plane of the bottom edge. The outer plate (10 in FIG. 1) is 4.10 inches high at the rear, measured from the end of the top flat to the bottom. The height of the inner plate (11 in FIG. 1) is 1 1/2 inches and extends beyond the outer plate (10 in FIG. 1) as shown in FIG. 1. Drilled holes are centered in the height of the inner plate (11 in FIG. 1). All holes (12 in FIG. 1) are 1/4 inch or larger corresponding to O.E.M. sponsons removed. The degree of slope of the top edge of the outer plate (10 in FIG. 1) will vary depending on the length of the plate (10 in FIG. 1).

Operation

As shown in FIGS. 3, 4 and 5 the outer plate (10 in FIG. 1) extends below the outer edge of the personal watercraft. This extension traps water as a rudder would, creating resistance against the plate. This lateral resistance stops the rear of the craft from sliding in the opposite direction in which the craft is being steered.

A very important and unique feature of the outer plate (10 in FIG. 1) is its shape. This unique shape helps to eliminate a secondary and very detrimental reaction known as "sticking" in the aircraft industry. This "sticking" reaction occurs when fluid forces are in effect, the same as in similar air movement.

As the outer plate moves laterally while in a turn, if it were perfectly rectangular, a low pressure area down the center of the plate would form. This is due to fluid circulation off of the top and bottom edges. This low pressure area creates a suction that "sticks" the plate to the water. When coming out of a turn and returning to a straight course the craft has to be oversteered to break the plate loose. At this point there is a brief period of loss of control. During high speed manuevers, especially during competition this could be disastrous.

The design of my outer plate (10 in FIG. 1) with no sides being parallel discourages the alignment of any fluid circulation. This substantially reduces the formation of a low pressure area on the plate. The "sticking" situation has been reduced by an estimated 60%.

To further deal with the remaining 40% of this adhesion we have manufactured a plate using a textured finish. This finish containing literally thousands of minute vortex generators all but eliminate any suction on the outside of the plates. This finish as used in the aircraft industry creates very little, if any parasitic drag and does not affect the straight ahead maximum speed of the craft.

Summary, Ramifications, and Scope

I believe that the reader may see that the relatively simple installation of these devices on a personal watercraft will greatly enhance the maneuverability of the craft. The additional safety of operation due to more accurate steering control should be considered a major attribute of this invention.

Although the preceeding description contains many specifications, these should not be construed as limitations on the scope of the invention, but rather as an exemplification of one preferred embodiment thereof. Many other variations are possible. For example the elimination of the textured surface would detune the operation of this device but it would remain viable even with a smooth surface on the outer plates.

Accordingly, the scope of the invention should be determined not by the embodiment illustrated, but by the appended claims and their legal equivalents.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2757629 *Nov 6, 1953Aug 7, 1956Harwill IncBoat stabilizers
US4159691 *Jul 12, 1977Jul 3, 1979Paxton Roland KMarine craft employing bow-wave lift
US4597348 *Jun 10, 1985Jul 1, 1986Otakar JonasDetachable keel for small boats
US5235926 *Jun 5, 1992Aug 17, 1993Jones Earl RAnti-skid device for flat-bottomed boats
US5237953 *Nov 23, 1990Aug 24, 1993Mannerfelt GoeranAccessory rail for boats
US5313907 *Mar 18, 1993May 24, 1994Hodges Christopher AExternal rail system for boat
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US5911190 *Jul 11, 1997Jun 15, 1999Light Wave, Ltd.Boat activated wave generator
US6067923 *Jul 8, 1998May 30, 2000Ratlieff, Jr.; William D.Turbulent stabilizing venturi system
US6105527 *Jun 16, 1998Aug 22, 2000Light Wave Ltd.Boat activated wake enhancement method and system
US6523489May 8, 2001Feb 25, 2003Bombardier Inc.Personal watercraft and off-power steering system for a personal watercraft
US6524146Jun 18, 2002Feb 25, 2003Bombardier Inc.Watercraft having auxiliary steering
US6546884Feb 22, 2002Apr 15, 2003Javier RodriguezJet propelled watercraft stabilizing system
US6546888Jun 22, 2001Apr 15, 2003Bombardier Inc.Removable stabilizing fin for a watercraft
US6675730Jul 16, 2002Jan 13, 2004Bombardier Inc.Personal watercraft having off-power steering system
US6675732Sep 12, 2001Jan 13, 2004Honda Giken Kogyo Kabushiki KaishaSponson for watercraft
US7210422Mar 8, 2004May 1, 2007Aluminum Chambered Boats Llc, Inc.Fin stabilizer to reduce roll for boats in turns method and apparatus
US7513204Mar 9, 2007Apr 7, 2009Aluminum Chambered Boats, Inc.Fin stabilizer to reduce roll for boats in turns method and apparatus
US8393287Nov 30, 2010Mar 12, 2013Bombardier Recreational Products Inc.Sponsons for a watercraft
WO2002022438A2 *Sep 12, 2001Mar 21, 2002Honda Motor Co LtdSponson for watercraft
WO2009070852A1 *Dec 5, 2008Jun 11, 2009John Gene FosterA watercraft stability control device
Classifications
U.S. Classification114/126, 114/283
International ClassificationB63B39/06, B63B35/73
Cooperative ClassificationB63B2001/186, B63B35/731, B63B39/06
European ClassificationB63B35/73B, B63B39/06
Legal Events
DateCodeEventDescription
May 17, 2005FPExpired due to failure to pay maintenance fee
Effective date: 20050318
Mar 18, 2005LAPSLapse for failure to pay maintenance fees
Oct 7, 2004REMIMaintenance fee reminder mailed
May 4, 2000FPAYFee payment
Year of fee payment: 4